EasyManua.ls Logo

Boeing 737-800 - Page 654

Boeing 737-800
1636 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
737 Flight Crew Operations Manual
Automatic Flight -
System Description
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
4.20.16 D6-27370-866-EGP
800 Feet Radio Altitude
The second A/P must be engaged in CMD by 800 feet RA to execute a dual
channel A/P approach. Otherwise, CMD engagement of the second A/P is
inhibited.
400 Feet Radio Altitude
The stabilizer is automatically trimmed an additional amount nose up. If the A/Ps
subsequently disengage, forward control column force may be required to hold the
desired pitch attitude.
If FLARE is not armed by approximately 350 feet RA, both A/Ps automatically
disengage.
Flare
The A/P flare maneuver starts at approximately 50 feet RA and is completed at
touchdown:
FLARE engaged is annunciated and F/D command bars retract.
the A/T begins retarding thrust at approximately 27 feet RA so as to
reach idle at touchdown. A/T FMA annunciates RETARD.
the A/T automatically disengages approximately 2 seconds after
touchdown.
the A/P must be manually disengaged after touchdown. Landing roll-out
is executed manually after disengaging the A/P.
Approach (APP) Mode Single A/P
A single A/P ILS approach can be executed by engaging only one A/P in CMD
after pushing the APP mode select switch. Single A/P approach operation is the
same as dual, with the following exceptions:
full automatic flare and touchdown capability is not available. FLARE
is not annunciated and stabilizer trim bias is not applied
YK981 - YQ456
if the pilot is flying manually but not following the approach flight
director guidance and then selects an autopilot CMD engagement, the
autopilot reverts to CWS for the pitch and/or roll mode.
YW273, YW274
if the pilot is flying manually but not following the approach flight
director guidance and then selects an autopilot CMD engagement, the
autopilot reverts to CWS for the pitch and/or roll mode. The approach
mode(s) will then re-arm.
A/P status of SINGLE CH is annunciated for the entire approach after
localizer capture
an A/P go–around is not available.
September 15, 2016

Table of Contents

Related product manuals